Bücher zum Thema „Rotari“
Geben Sie eine Quelle nach APA, MLA, Chicago, Harvard und anderen Zitierweisen an
Machen Sie sich mit Top-50 Bücher für die Forschung zum Thema "Rotari" bekannt.
Neben jedem Werk im Literaturverzeichnis ist die Option "Zur Bibliographie hinzufügen" verfügbar. Nutzen Sie sie, wird Ihre bibliographische Angabe des gewählten Werkes nach der nötigen Zitierweise (APA, MLA, Harvard, Chicago, Vancouver usw.) automatisch gestaltet.
Sie können auch den vollen Text der wissenschaftlichen Publikation im PDF-Format herunterladen und eine Online-Annotation der Arbeit lesen, wenn die relevanten Parameter in den Metadaten verfügbar sind.
Sehen Sie die Bücher für verschiedene Spezialgebieten durch und erstellen Sie Ihre Bibliographie auf korrekte Weise.
Kadiĭski, T︠S︡vi︠a︡tko. Rotari v Sofii︠a︡: Legenda i deĭstvitelnost. Sofia]: Kolbis, 2000.
Den vollen Inhalt der Quelle findenPavlović, Momčilo. Rotari klub Subotica: 1929-1941, 1997-2008 = Szabadkai Rotary Klub = Szabadkai Rotary Klub. Subotica: Rotari klub, 2008.
Den vollen Inhalt der Quelle findenPolazzo, Marco. Pietro Rotari: Pittore veronese del Settecento (1707-1762). Negrar (Verona): Il Segno, 1990.
Den vollen Inhalt der Quelle findenLa vita quotidiana dei Longobardi ai tempi di re Rotari. Imola (Bologna): G. Angelini, 2007.
Den vollen Inhalt der Quelle findenIl Settecento a Verona: Tiepolo, Cignaroli, Rotari : la nobiltà della pittura. Cinisello Balsamo (Milano): Silvana, 2011.
Den vollen Inhalt der Quelle findenBrooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Den vollen Inhalt der Quelle findenBrooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. Hampton, Va: Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenRalph, Jolly J., Marcolini Michael A und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Helicopter main-rotor noise: Determination of source contributions using scaled model data. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Den vollen Inhalt der Quelle findenBrooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Den vollen Inhalt der Quelle findenRunyan, Harry L. Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight. Washington: NASA, 1985.
Den vollen Inhalt der Quelle findenH, Tai, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Hrsg. Compressible, unsteady, lifting-surface theory for a helicopter rotor in forward flight. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Den vollen Inhalt der Quelle findenWilbur, Matthew L. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Den vollen Inhalt der Quelle findenRiley, M. J. Measurements of the performance of a helicopter swept tip rotor in flight. [S.l.]: [s.n.], 1986.
Den vollen Inhalt der Quelle findenWeber, Gregor J. M. Pietro Graf Rotari in Dresden: Ein italienischer Maler am Hof König Augusts III. : Bestandskatalog anlässlich der Ausstellung im Semperbau, 9. November 1999-9. Januar 2000. Emstetten/Dresden: Edition Imorde, 1999.
Den vollen Inhalt der Quelle findenR, Johnson Wayne, und United States. National Aeronautics and Space Administration., Hrsg. Navier-Stokes calculations for a highly-twisted rotor near stall. [Washington, D.C: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenE, Teske Milton, Quackenbush Todd R, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. und Ames Research Center, Hrsg. A new methodology for free wake analysis using curved vortex elements. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Den vollen Inhalt der Quelle findenR, Johnson Wayne, und United States. National Aeronautics and Space Administration., Hrsg. Navier-Stokes calculations for a highly-twisted rotor near stall. [Washington, D.C: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenR, Johnson Wayne, und United States. National Aeronautics and Space Administration., Hrsg. Navier-Stokes calculations for a highly-twisted rotor near stall. [Washington, D.C: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenKorea) Hanyang Rotʻari Kʻŭllŏp (Seoul. Hanyang Rotʻari Kʻŭllŏp 30-yŏnsa: Rotary Club of Hanyang thirty years of service. Seoul, Korea: Hanyang Rotʻari Kʻŭllŏp, 1985.
Den vollen Inhalt der Quelle findenRobinson, Christopher S. Modeling and analysis of helicopter ground resonance utilizing symbolic processing and dynamic simulation software. Monterey, Calif: Naval Postgraduate School, 1997.
Den vollen Inhalt der Quelle findenInternational Symposium on Transport Phenomena and Dynamics of Rotating Machinery (3rd 1990 Honolulu, Hawaii). Rotating machinery--transport phenomena: Proceedings of the Third International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-3). Washington: Hemisphere Pub. Corp., 1992.
Den vollen Inhalt der Quelle findenInternational Symposium on Transport Phenomena and Dynamics of Rotating Machinery (3rd 1990 Honolulu, Hawaii). Rotating machinery--dynamics: Proceedings of the Third International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-3). Washington: Hemisphere Pub. Corp., 1992.
Den vollen Inhalt der Quelle findenBeach, Bert Beverly. Rotating the world with Rotary: Personal diary of a visiting Rotarian. [Maryland?]: B.B. Beach, 1991.
Den vollen Inhalt der Quelle findenKʻŭllŏp, Migŭm Rotʻari. Migŭm Rotʻari simnyŏnsa: History of Rotary for 10 years serviced in Migum, 1981--1991. Kyŏnggi-do Migŭm-si: Migŭm Rotʻari Kʻŭllŏp, 1991.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. A study of rotor broadband noise mechanisms and helicopter tail rotor noise. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Den vollen Inhalt der Quelle findenEgolf, T. Alan. A full potential analysis with realistic wake influence for helicopter rotor airload prediction. Moffett Field, Calif: Ames Research Center, 1987.
Den vollen Inhalt der Quelle findenKitaplioglu, Cahit. Analysis of small-scale rotor hover performance data. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Den vollen Inhalt der Quelle findenColeman, Colin P. A survey of theoretical and experimental coaxial rotor aerodynamic research. Washington, D.C: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. A survey of theoretical and experimental coaxial rotor aerodynamic research. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.
Den vollen Inhalt der Quelle findenCenter, Ames Research, Hrsg. A survey of theoretical and experimental coaxial rotor aerodynamic research. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.
Den vollen Inhalt der Quelle findenCooper, Fiona. Rotary Spokes. London, England: Brilliance Books, 1988.
Den vollen Inhalt der Quelle findenDudaș, Vasile. Pavel Rotariu. Timișoara: Excelsior Art, 2002.
Den vollen Inhalt der Quelle findenChen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.
Den vollen Inhalt der Quelle findenChen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. Moffett Field, Calif: Ames Research Center, 1989.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight: An experimental and analytical investigation of isolated rotor-flap-lag stability in forward flight. Boca Raton, FL: Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering, 1986.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight: Final technical report under NASA-Ames cooperative agreement no. NCC 2-361 (August 1, 1985 - July 31, 1987). Boca Raton, FL: Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering, 1987.
Den vollen Inhalt der Quelle findenKhánh, Nguyẽ̂n, und Ames Research Center, Hrsg. Aeroelastic stability of a full-scale hingeless rotor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.
Den vollen Inhalt der Quelle findenKhanh, Nguyen, und Ames Research Center, Hrsg. Aeroelastic stability of a full-scale hingeless rotor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.
Den vollen Inhalt der Quelle findenJ, Mack, Mount R und United States. National Aeronautics and Space Administration., Hrsg. Two rotor stratified charge rotary engine (SCRE) engine system technology evaluation. [Washington, D.C: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenUnited States. Army. Aerostructures Directorate. und Langley Research Center, Hrsg. Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Den vollen Inhalt der Quelle findenHamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. Moffett Field, Calif: Ames Research Center, 1990.
Den vollen Inhalt der Quelle findenHamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Den vollen Inhalt der Quelle findenM, Kufeld Robert, Ames Research Center und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Den vollen Inhalt der Quelle findenM, Kufeld Robert, Ames Research Center und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Den vollen Inhalt der Quelle finden